Sensorless Position Estimator for Reciprocating Linear Actuator Hardware
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This six-month SBIR Phase I project under solicitation NASA-SBIR-185323 focuses on developing and validating a model-based dynamic piston position observer for reciprocating linear actuators. By utilizing existing coil current and terminal voltage monitoring, the proposed software-based estimator eliminates the need for additional sensors or current injection hardware. This approach aims to improve the reliability and power density of NASA Radioisotope Power Systems by enabling precise control over piston amplitude, correcting mean position drift, and coordinating dual-opposed converters to minimize vibration. The technology is compatible with moving-magnet and low-inductance moving coil alternator-based converters, with potential applications ranging from space probes and landers to cryocoolers and zero-boiloff fluid storage. Beyond aerospace, the sensorless position estimation intellectual property has broader commercial viability for industrial actuators, automotive suspensions, and terrestrial remote power systems. The project is managed by the NASA SBIR/STTR Program and is designated as a total small business set-aside.
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Place of Performance
Cleveland, OH, 44135, USASet-Aside
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Benefits: Our sensorless piston position estimator can support dynamic radioisotope power system (RPS) Stirling convertors at any power level – from tens of watts to kilowatts. According to the solicitation, NASA is considering using Stirling convertors “to power science missions for the Moon and other solar system bodies of interest… for use on space probes, landers, and rovers, battery chargers, sensors, etc.” We understand that many of the RPS convertor controllers developed by NASA already monitor coil current and terminal voltage. Therefore, controllers equipped with microprocessors could, in principle, be upgraded to host our position estimation algorithms without the need for additional sensors or current injection hardware, thereby enhancing overall system reliability, particularly during extended missions. Furthermore, utilizing information about piston position (including amplitude, offset, and phase) could improve specific power density by allowing the controller to operate more safely closer to the physical limits of piston travel while synchronizing with other converters and vibration absorbers. It might even be feasible to implement our sensorless position observer for the linear actuator of an active (driven) vibration absorber, potentially eliminating the need for a separate accelerometer. Our piston position observer is suitable for moving-magnet-based converters and the low-power, low-inductance moving coil alternator-based converter developed by NASA-GRC. Additionally, our position estimator could be utilized in NASA cryocooler applications to directly cool space sensors and reliquefy vapor for zero-boiloff fluid storage. The estimator could also apply to linear gas compressor/ liquid transfer pumps or other linear actuators applications. Our position estimator could support Stirling convertors for domestic micro-cogeneration appliances, portable power and battery charging systems, and terrestrial remote power applications requiring high reliability (e.g., navigation or communications equipment at off-grid sites). Our estimator IP could also provide sensorless piston position feedback capability to cryocooler controllers, enhancing performance and reliability. The global market for Stirling cryocoolers is expected to reach $7.4 billion (USD) by 2026, with a compound annual growth rate of 10.5% from 2021 to 2026. In the U.S., the Stirling cryocooler segment is projected to experience the highest growth rate among all cryocooling technologies during the forecast period 2022-2030. Through the I-Corps interviews from our last SBIR project, we identified the potential relevance of our sensorless position estimation IP for industrial actuators, including solenoids and valves, closed-loop control of moving-coil speakers, and active automotive suspensions.
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